Outlet nozzle for gases would mean, in particular, thrust nozzle for rocket engines

• 1. 用于火箭发动机的在喷嘴的固定部与移动部之间设置有密封装置的燃烧气体排放喷嘴 [P] . 中国专利： CN105408610B . 2018.04.20
• 2. 用于火箭发动机的在喷嘴的固定部与移动部之间设置有密封装置的燃烧气体排放喷嘴 [P] . 中国专利： CN105408610A . 2016-03-16
• 3. Outlet nozzle for gases would mean, in particular, thrust nozzle for rocket engines [P] . 德国专利： DE000002054919A . 1971-07-22

  机译： 气体的出口喷嘴尤其意味着火箭发动机的推力喷嘴

• 4. Outlet nozzle for gases would mean, in particular, thrust nozzle for rocket engines [P] . 德国专利： DE2054919A1 . 1971-07-22

  机译： 气体的出口喷嘴尤其意味着火箭发动机的推力喷嘴

• 5. Design and arrangement of an inlet ring or outlet collecting ring for thrust nozzles or combustion chambers of rocket engines, in particular flue signal drive works as a function of the rockets [P] . 德国专利： DE1751180A1 . 1971-04-29

  机译： 用于火箭发动机的推力喷嘴或燃烧室的入口环或出口收集环的设计和布置，尤其是烟道信号驱动器的功能取决于火箭

• 1. Center of rotation estimation for rocket nozzle by infrared reflective makers and image sequences [J] . ZHANG Ling-fei, CHEN Gang, YE Dong, 哈尔滨工业大学学报（英文版） . 2011,第002期
• 2. Center of rotation estimation for rocket nozzle by infrared reflective makers and image sequences [J] . ZHANG Ling-fei, CHEN Gang, YE Dong, 哈尔滨工业大学学报：英文版 . 2011,第002期
• 3. THRUST AUGMENTATION NOZZLE (TAN) CONCEPT FOR ROCKET ENGINE BOOSTER APPLICATIONS [C] . Scott Forde, Mel Bulman, Todd Neill 56th International Astronautical Congress 2005 vol.7 . 2005
• 4. Thrust Augmented Nozzle for a Hybrid Rocket with a Helical Fuel Port [D] . Marshall, Joel H. 2018
• 5. Effects of Cavity on the Performance of Dual Throat Nozzle During the Thrust-Vectoring Starting Transient Process [O] . Rui Gu, Jinglei Xu -1
• 6. Rocket engine thrust vector control by detonation product injection into the supersonic portion of the nozzle [O] . S.S. Vasyliv, H.O. Strelnykov 2020
• 7. Performance and Thrust-to-Weight Optimization of the Dual-Expander Aerospike Nozzle Upper Stage Rocket Engine. [R] . Hall, J. N., Hartsfield, C. R., Simmons, J. R., 2012

• 1. Based on Fluent Numerical Calculation of Refractive Index on Rocket Engine Nozzle Plume [J] . Qiangfeng Huang ,Xiong Wan ,Zhimin Zhang . 光学与光子学期刊（英文） . 2013,第2期
• 2. Overview of Physical and Chemical, Operational Properties of Nitrous Oxide Used as a Propellant for Low-thrust Rocket Engines [J] . A.A.Boryaev . 火炸药学报 . 2019,第1期
• 3. Energy consumption of large space atrium under nozzle outlet during winter season [J] . 赵惠忠 ,林志芬 ,陈飞 . 中南大学学报 . 2009,第0S1期
• 4. 水下缝式喷嘴喷吹气体产生的气体分散现象和搅拌特性研究 [C] . KEIJI OKUMURA ,MASAMICHI SANO . 2000年亚洲钢铁大会 . 2000
• 5. 喷嘴孔数及其布置情况对汽油直喷喷嘴闪沸喷雾-环境气体相互作用影响的研究 [A] . 佟斯日古楞 . 2016